Download or read book Asymptotic Hypersonic Flow Theory for Blunted Slender Cones and Wedges written by John W. Ellinwood and published by . This book was released on 1966 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: Inviscid hypersonic flow over slender, unyawed circular cones and wedges has been perturbed for the effect of nose bluntness far behind the nose. The resulting singular-perturbation problem is solved with matched inner and outer asymptotic expansions. For both plane and axisymmetric flows, the leading perturbation in surface pressure is an eigensolution which varies as the real part of downstream distance raised to complex powers. The imaginary parts of all exponents are multiples of a fundamental frequency, and all harmonics decay at a rate which depends on Mach number, specific heat ratio and body geometry. For blunted wedges, the perturbation equations are integrated in closed form generally. The displacement of the shock asymptote relative to the body asymptote was determined without approximation. For blunted cones, it is shown that logarithms do not appear where the afterbody is specified, unlike the inverse problem of flow behind a hyperboloidal shock. Three limiting axisymmetric cases are considered: infinite Mach number, specific heat ratio of unity, and a combination of these known as the NEWTONIAN SLENDER BODY limit. (Author).

Download or read book Asymptotic Behavior of Hypersonic Flow Over Blunted Slender Wedges written by Wilhelm Schneider and published by . This book was released on 1968 with total page 2 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Theory of Entropy Layers and Nose Bluntness in Hypersonic Flow written by James Kiyoshi Yakura and published by . This book was released on 1961 with total page 186 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 776 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Asymptotic Theory of the Blunted Wedge at Hypersonic Speeds written by R. Gopinath and published by . This book was released on 1968 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Technical Note written by and published by . This book was released on 1960 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1992 with total page 1572 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NAL Technical Note written by and published by . This book was released on 1967 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Hypersonic Inviscid Flow written by Wallace D. Hayes and published by Courier Corporation. This book was released on 2012-07-13 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt: Unified, self-contained view of nonequilibrium effects, body geometries, and similitudes available in hypersonic flow and thin shock layer; appropriate for graduate-level courses in hypersonic flow theory. 1966 edition.

Download or read book Hypersonic Flow Theory Inviscid flows written by Wallace Dean Hayes and published by . This book was released on 1966 with total page 632 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Hypersonic Rarefied Flow Over Sharp Slender Cones written by Marvin I. Kussoy and published by . This book was released on 1972 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Drag, heat transfer, and number flux were measured on sharp cones in the near free, molecule flow regime, and the results were compared with available Monte Carlo calculations. In general, the calculations predicted the magnitude of the data; however, the heat transfer and drag increased with increasing Knudsen number at a faster rate than predicted. Also the drag coefficients measured for the slender cones at high Knudsen number were higher than predicted for free molecule flow. These disagreements between theory and experiment could possibly be attributed to the simplicity of the surface interaction laws assumed in the theory. Reynolds analogy factors obtained from the experimental measurements agreed with free-molecule values and also with that obtained by the Monte Carlo technique.

Download or read book Effects of Angle of Attack and Bluntness on the Hypersonic Flow Over a 15 semiapex Cone in Helium written by Joseph W. Cleary and published by . This book was released on 1970 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Experimental and Theoretical Investigation of the Pressure Distribution and Flow Fields of Blunted Cones at Hypersonic Mach Number written by Joseph W. Cleary and published by . This book was released on 1965 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effect of Body Perturbations on Hypersonic Flow Over Slender Power Law Bodies written by Harold Mirels and published by . This book was released on 1959 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Approximate Analytical Solutions for Hypersonic Flow Over Slender Power Law Bodies written by Harold Mirels and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Technical Report written by and published by . This book was released on 1959 with total page 344 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Research Review written by and published by . This book was released on 1970 with total page 296 pages. Available in PDF, EPUB and Kindle. Book excerpt: